Fixed-wing unmanned aerial vehicle stable in landing
The fixed-wing unmanned aerial vehicle comprises a fuselage, an empennage, wings and propellers, the two wings are oppositely arranged on the two sides of the middle of the fuselage, the wings comprise the inner wing, the middle wing and the outer wing, the inner wing is connected to the fuselage, t...
Gespeichert in:
| Hauptverfasser: | , , , , , , , , , |
|---|---|
| Format: | Patent |
| Sprache: | chi ; eng |
| Schlagworte: | |
| Online-Zugang: | Volltext bestellen |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | |
|---|---|
| container_issue | |
| container_start_page | |
| container_title | |
| container_volume | |
| creator | LIU LIANGLIANG WU JUN CHEN HAIFENG ZANG LIN FU YIFENG YUE YANGE XU ZHIHUI ZHANG YUANYUAN DU GUANGHUI GUO XUENI |
| description | The fixed-wing unmanned aerial vehicle comprises a fuselage, an empennage, wings and propellers, the two wings are oppositely arranged on the two sides of the middle of the fuselage, the wings comprise the inner wing, the middle wing and the outer wing, the inner wing is connected to the fuselage, the middle wing is slidably sleeved with the inner wing in the length direction of the inner wing, and the propellers are arranged in the middle of the fuselage. The outer wing is slidably sleeved with the middle wing in the length direction of the middle wing, the propeller is fixedly arranged on the lower side of the end, away from the inner wing, of the middle wing, the empennage is slidably arranged on the rear portion of the fuselage in the length direction of the fuselage, and a tail rotor is arranged at the end, away from the fuselage, of the empennage. Wing unfolding mechanisms are arranged in the wings, and extending mechanisms are arranged between the empennages and the fuselage. The invention aims to solv |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN116552841A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN116552841A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN116552841A3</originalsourceid><addsrcrecordid>eNrjZDBxy6xITdEtz8xLVyjNy03My0tNUUhMLcpMzFEoS83ITM5JVSguSUwCUpl5CjmJeSlAlTwMrGmJOcWpvFCam0HRzTXE2UM3tSA_PrW4IDE5NS-1JN7Zz9DQzNTUyMLE0NGYGDUAEvUsgg</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Fixed-wing unmanned aerial vehicle stable in landing</title><source>esp@cenet</source><creator>LIU LIANGLIANG ; WU JUN ; CHEN HAIFENG ; ZANG LIN ; FU YIFENG ; YUE YANGE ; XU ZHIHUI ; ZHANG YUANYUAN ; DU GUANGHUI ; GUO XUENI</creator><creatorcontrib>LIU LIANGLIANG ; WU JUN ; CHEN HAIFENG ; ZANG LIN ; FU YIFENG ; YUE YANGE ; XU ZHIHUI ; ZHANG YUANYUAN ; DU GUANGHUI ; GUO XUENI</creatorcontrib><description>The fixed-wing unmanned aerial vehicle comprises a fuselage, an empennage, wings and propellers, the two wings are oppositely arranged on the two sides of the middle of the fuselage, the wings comprise the inner wing, the middle wing and the outer wing, the inner wing is connected to the fuselage, the middle wing is slidably sleeved with the inner wing in the length direction of the inner wing, and the propellers are arranged in the middle of the fuselage. The outer wing is slidably sleeved with the middle wing in the length direction of the middle wing, the propeller is fixedly arranged on the lower side of the end, away from the inner wing, of the middle wing, the empennage is slidably arranged on the rear portion of the fuselage in the length direction of the fuselage, and a tail rotor is arranged at the end, away from the fuselage, of the empennage. Wing unfolding mechanisms are arranged in the wings, and extending mechanisms are arranged between the empennages and the fuselage. The invention aims to solv</description><language>chi ; eng</language><subject>AIRCRAFT ; AVIATION ; COSMONAUTICS ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2023</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20230808&DB=EPODOC&CC=CN&NR=116552841A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25555,76308</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20230808&DB=EPODOC&CC=CN&NR=116552841A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>LIU LIANGLIANG</creatorcontrib><creatorcontrib>WU JUN</creatorcontrib><creatorcontrib>CHEN HAIFENG</creatorcontrib><creatorcontrib>ZANG LIN</creatorcontrib><creatorcontrib>FU YIFENG</creatorcontrib><creatorcontrib>YUE YANGE</creatorcontrib><creatorcontrib>XU ZHIHUI</creatorcontrib><creatorcontrib>ZHANG YUANYUAN</creatorcontrib><creatorcontrib>DU GUANGHUI</creatorcontrib><creatorcontrib>GUO XUENI</creatorcontrib><title>Fixed-wing unmanned aerial vehicle stable in landing</title><description>The fixed-wing unmanned aerial vehicle comprises a fuselage, an empennage, wings and propellers, the two wings are oppositely arranged on the two sides of the middle of the fuselage, the wings comprise the inner wing, the middle wing and the outer wing, the inner wing is connected to the fuselage, the middle wing is slidably sleeved with the inner wing in the length direction of the inner wing, and the propellers are arranged in the middle of the fuselage. The outer wing is slidably sleeved with the middle wing in the length direction of the middle wing, the propeller is fixedly arranged on the lower side of the end, away from the inner wing, of the middle wing, the empennage is slidably arranged on the rear portion of the fuselage in the length direction of the fuselage, and a tail rotor is arranged at the end, away from the fuselage, of the empennage. Wing unfolding mechanisms are arranged in the wings, and extending mechanisms are arranged between the empennages and the fuselage. The invention aims to solv</description><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDBxy6xITdEtz8xLVyjNy03My0tNUUhMLcpMzFEoS83ITM5JVSguSUwCUpl5CjmJeSlAlTwMrGmJOcWpvFCam0HRzTXE2UM3tSA_PrW4IDE5NS-1JN7Zz9DQzNTUyMLE0NGYGDUAEvUsgg</recordid><startdate>20230808</startdate><enddate>20230808</enddate><creator>LIU LIANGLIANG</creator><creator>WU JUN</creator><creator>CHEN HAIFENG</creator><creator>ZANG LIN</creator><creator>FU YIFENG</creator><creator>YUE YANGE</creator><creator>XU ZHIHUI</creator><creator>ZHANG YUANYUAN</creator><creator>DU GUANGHUI</creator><creator>GUO XUENI</creator><scope>EVB</scope></search><sort><creationdate>20230808</creationdate><title>Fixed-wing unmanned aerial vehicle stable in landing</title><author>LIU LIANGLIANG ; WU JUN ; CHEN HAIFENG ; ZANG LIN ; FU YIFENG ; YUE YANGE ; XU ZHIHUI ; ZHANG YUANYUAN ; DU GUANGHUI ; GUO XUENI</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN116552841A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2023</creationdate><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>LIU LIANGLIANG</creatorcontrib><creatorcontrib>WU JUN</creatorcontrib><creatorcontrib>CHEN HAIFENG</creatorcontrib><creatorcontrib>ZANG LIN</creatorcontrib><creatorcontrib>FU YIFENG</creatorcontrib><creatorcontrib>YUE YANGE</creatorcontrib><creatorcontrib>XU ZHIHUI</creatorcontrib><creatorcontrib>ZHANG YUANYUAN</creatorcontrib><creatorcontrib>DU GUANGHUI</creatorcontrib><creatorcontrib>GUO XUENI</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>LIU LIANGLIANG</au><au>WU JUN</au><au>CHEN HAIFENG</au><au>ZANG LIN</au><au>FU YIFENG</au><au>YUE YANGE</au><au>XU ZHIHUI</au><au>ZHANG YUANYUAN</au><au>DU GUANGHUI</au><au>GUO XUENI</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Fixed-wing unmanned aerial vehicle stable in landing</title><date>2023-08-08</date><risdate>2023</risdate><abstract>The fixed-wing unmanned aerial vehicle comprises a fuselage, an empennage, wings and propellers, the two wings are oppositely arranged on the two sides of the middle of the fuselage, the wings comprise the inner wing, the middle wing and the outer wing, the inner wing is connected to the fuselage, the middle wing is slidably sleeved with the inner wing in the length direction of the inner wing, and the propellers are arranged in the middle of the fuselage. The outer wing is slidably sleeved with the middle wing in the length direction of the middle wing, the propeller is fixedly arranged on the lower side of the end, away from the inner wing, of the middle wing, the empennage is slidably arranged on the rear portion of the fuselage in the length direction of the fuselage, and a tail rotor is arranged at the end, away from the fuselage, of the empennage. Wing unfolding mechanisms are arranged in the wings, and extending mechanisms are arranged between the empennages and the fuselage. The invention aims to solv</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | chi ; eng |
| recordid | cdi_epo_espacenet_CN116552841A |
| source | esp@cenet |
| subjects | AIRCRAFT AVIATION COSMONAUTICS PERFORMING OPERATIONS TRANSPORTING |
| title | Fixed-wing unmanned aerial vehicle stable in landing |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-14T18%3A42%3A17IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=LIU%20LIANGLIANG&rft.date=2023-08-08&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3ECN116552841A%3C/epo_EVB%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true |